UJI TERBANG PESAWAT UAV V-SKY 14 NEXT GENERATION

ZULFADIN HANAFI, IHYA (2022) UJI TERBANG PESAWAT UAV V-SKY 14 NEXT GENERATION. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

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Abstract

The V-Sky 14 Next Generation UAV is a remotely controlled unmanned aircraft, to design an aircraft must start from several stages starting from initial design, detail design, manufacturing and flight testing. This aircraft has reached the initial design, detail design and manufacturing stage. Due to the stages that have not been carried out in this design, namely flight testing and this important in designing a UAV aircraft, this flight test was carried out, this aims to determine the performance of the V-Sky 14 Next Generation UAV aircraft to obtain range and endurance values at the V-Sky 14 Next Generation. This is useful for knowing the performance of the V-Sky 14 Nest Generation UAV aircraft. The method used is a theoretical calculation method with test calculation in the field. The V-Sky 14 Next Generation UAV aircraft is an aircraft that has been modifed from the previous model, namely the V-SKY 14 UAV. The aircraft has VTOL capability and electrically powered, with wingspan 1,713125m with fuselage length of 650 mm and uses 5 engine brushless, 4 engine for VTOL mode and 1 engine for cruise mode and using Pixhawk 2.4.8 flight controller. Based on the result of theoritical calculation, it can be seen that the range value is 0,66756 km or 667,56 m and the endurance 0,03636 hour or 130, 896 second. In addition, the range and endurance values were also obtained from field test whare the respective values ware 0,2475 km or 247,5 m and 0,0134 hour or 48,442 seconds.

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